Mach Architect: Learn Compressible Flow by Designing Nozzles
·4 min read
At γ = 1.4 the choke ratio is 0.5283 and the M = 2 area ratio is about 1.6875. Back pressure between those two parks a normal shock inside the nozzle.
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At γ = 1.4 the choke ratio is 0.5283 and the M = 2 area ratio is about 1.6875. Back pressure between those two parks a normal shock inside the nozzle.
Related tags